The Evaluation Tests of the Attitude Control System of the 50-kg Micro Satellite RISING-2
スポンサーリンク
概要
- 論文の詳細を見る
The 50-kg class micro satellite RISING-2 is now under development by Tohoku University and Hokkaido University. The development is at Flight Model phase and some components are tested to evaluate its specifications. In this paper, the endurance tests using vacuum chamber and thermal test chamber in Tohoku University are described. There was no problem in those tests. In addition, the attitude control accuracy of the RISING-2 was analyzed in the simulation. This simulation based on component specifications and also included noise data. The results show the pointing error angle was less than required error angle.
- THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCESの論文
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES | 論文
- Study on Ignition and Electron Emission Characteristics of Inductively Coupled Plasma Cathode
- Research and Development of a Debris Removal Method Using Interaction between Space and Electrode with Applied Voltage
- Disaster Monitoring Using ALOS/PALSAR Data
- Design and Experimental Validation of Inter-Satellite Link System for Formation Flight SCOPE Mission
- Magnetic Inflation of Magnetic Plasma Sail by One Component Plasma Simulation